CA2911765C - Systems and methods for non-destructive evaluation of molds and crucibles used in investment casting - Google Patents

Systems and methods for non-destructive evaluation of molds and crucibles used in investment casting Download PDF

Info

Publication number
CA2911765C
CA2911765C CA2911765A CA2911765A CA2911765C CA 2911765 C CA2911765 C CA 2911765C CA 2911765 A CA2911765 A CA 2911765A CA 2911765 A CA2911765 A CA 2911765A CA 2911765 C CA2911765 C CA 2911765C
Authority
CA
Canada
Prior art keywords
crucible
mold
ceramic
refractory oxide
scanning device
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CA2911765A
Other languages
French (fr)
Other versions
CA2911765A1 (en
Inventor
Bernard Patrick Bewlay
Jonathan Sebastian Janssen
Christopher Allen Nafis
Clifford Bueno
Krzysztof LESNICKI
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of CA2911765A1 publication Critical patent/CA2911765A1/en
Application granted granted Critical
Publication of CA2911765C publication Critical patent/CA2911765C/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00—Computer-aided design [CAD]
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B11/00—Measuring arrangements characterised by the use of optical techniques
    • G01B11/24—Measuring arrangements characterised by the use of optical techniques for measuring contours or curvatures
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B21/00—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
    • G01B21/02—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring length, width, or thickness
    • G01B21/04—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring length, width, or thickness by measuring coordinates of points
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B21/00—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
    • G01B21/20—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring contours or curvatures, e.g. determining profile

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Evolutionary Computation (AREA)
  • General Engineering & Computer Science (AREA)
  • Geometry (AREA)
  • Computer Hardware Design (AREA)
  • Length Measuring Devices By Optical Means (AREA)
  • Architecture (AREA)
  • Software Systems (AREA)
  • Crystals, And After-Treatments Of Crystals (AREA)
  • Length Measuring Devices With Unspecified Measuring Means (AREA)
  • Analysing Materials By The Use Of Radiation (AREA)

Abstract

The present disclosure relates to systems and methods useful for non-destructive evaluation (NDE) of molds and crucibles used in investment casting processes, including, without limitation, for producing aircraft engines, land-based turbine engines, and the like. According to one aspect, the present disclosure provides a system for non-destructive evaluation that includes a support, a 3D scanning device, and a computer component. According to another aspect, the present disclosure provides a method for non-destructive evaluation that includes the steps of: providing a system for non-destructive evaluation of a mold or crucible according to the present disclosure; securing a mold or crucible to the support of the system; and operating the 3D scanning device of the system in conjunction with the computer component in order to create a 3D structure difference map that indicates whether the mold or crucible falls within or outside a desired structural integrity parameter range.

Description

SYSTEMS AND METHODS FOR NON-DESTRUCTIVE EVALUATION OF MOLDS
AND CRUCIBLES USED IN INVESTMENT CASTING
BACKGROUND
[0001] The present disclosure relates to systems and methods useful for non-destructive evaluation (NDE) of molds and crucibles used in investment casting processes, including, without limitation, for producing aircraft engines, land-based turbine engines, and the like.
[0002] Molds and crucibles are commonly used in making components and parts for high performance devices such as aircraft and land-based turbine engines.
Uniformity and structural integrity of such molds and crucibles are important in maintaining quality control in investment casting processes. Control of the full volume geometry and the wall thickncss of investment casting molds and crucibles is important to ensure structural integrity of the mold or crucible and to prevent leaks occur during melting and casting. X-ray technology has been used to analyze the structural integrity of molds and crucibles. However, such X-ray techniques require highly specialized personnel and equipment, and generally more time-consuming than is permissible for a manufacturing environment. Therefore, there remains a need for practical techniques for inspecting the full volume geometry or wall thickness of a mold or crucible in a non-destructive manner prior to melting and casting.
[0003] The thickness of the wall is important because it has a major effect on the strength of the ceramic shell component. For example, if the thickness of the wall of the ceramic shell component falls below a minimum threshold value, the strength of the component falls below the minimum acceptable strength, and the liquid metal can leak from the crucible or mold. In some cases this leakage can result in a casting failure. Accordingly, wall thickness is a critical parameter of melting crucibles and casting molds, as thickness below a specification limit increase the likelihood of part loss during the casting operation.
[0004] There are current practices to check the wall thickness of crucibles. One current practice is to sample crucibles on a low-frequency basis. The measurement process involves installing the crucible into a fixture with point contacts on the internal face. Measurements are made with a dial indicator on or about points on the surface. After these measurements are made, the crucible must be discarded because the point-contacts damage the contacting surface of the crucible.
100051 Induction melting generally involves heating a metal in a crucible made from a non-conductive refractory alloy oxide until the charge of metal within the crucible is melted to liquid form (see, e.g., U.S. Patent No. 8,048,365 to Bewlay et al.). When melting highly reactive metals such as titanium or titanium alloys, vacuum induction melting using cold wall or graphite crucibles can be employed instead of oxide based ceramic crucibles.
Difficulties can arise when melting highly reactive alloys, such as titanium alloys, as a result of the reactivity of the elements in the alloy at the temperatures used for melting. While most induction melting systems use refractory oxides for crucibles in the induction furnace, alloys such as titanium aluminide are so highly reactive that they can attack the refractory oxides present in the crucible and the titanium alloy becomes contaminated. For example, ceramic crucibles are typically avoided because the highly reactive alloys can react with the crucible and contaminate the alloy, with oxygen for example. Similarly, if graphite crucibles are employed, both the titanium and titanium aluminide based alloys can dissolve carbon from the crucible into the titanium alloy, thereby resulting in contamination and loss of mechanical properties of the resulting article.
[0006] Cold crucible melting offers advantages for processing highly reactive alloys, but it also has a number of technical and economic limitations, including low superheat, yield losses due to skull formation, high power requirements, and limited melt capacity.
Any reaction between the molten alloy and the crucible will tend to deteriorate the properties of the casting.
The deterioration can be as simple as poor surface finish due to gas bubbles, or worse, the chemistry, microstructure, and properties of the casting can be compromised.
[0007] Accordingly, it is important to have inspection techniques in place to ensure the production of high quality crucibles for use in melting the metal or metal alloy. In one example, the inspection techniques are applied to ceramic crucibles used for highly reactive alloys, as the ceramic crucibles are less susceptible to contamination and pose fewer technical and economic limitations than current techniques. For example, rather than destructive sampling based inspection techniques, there is a need for inspection technologies that are non-destructive so as to preserve yields and that are effective to enable fast and efficient inspection.
[0008] The present systems and methods are directed to overcoming these and other deficiencies in the art.
SUMMARY
[0009] The present disclosure relates to systems and methods usefill for non-destructive evaluation (NDE) of molds and crucibles used in investment casting processes, including, without limitation, for use in producing components for aircraft engines, land-based turbine engines, and the like.
[0010] According to one aspect, the present disclosure provides a system for non-destructive evaluation of a mold or crucible. The system includes a support, a three-dimensional (3D) scanning device, and a computer component. The support comprises a fixture for securing a mold or crucible of interest in place for non-destructive evaluation, with the fixture comprising a mount portion onto which the mold or crucible is secured. The 3D scanning device is effective for scanning an outer surface of a target region of the mold or crucible in order to generate a 3D
structure of the scanned outer surface of the target region. The computer component is operably connected to the 3D scanning device and effective to create a difference map between the 3D
structure of the scanned outer surface of the target region of the mold or crucible and a 3D
structure of a reference object corresponding to an inner surface of a nominal model of the same target region of the mold or crucible. The difference map indicates whether the mold or crucible falls within or outside a desired structural integrity parameter range. In one embodiment, the support further comprises a locating mechanism for positioning the mold or crucible in a repeatable orientation on the support and maintaining the mold or crucible in that orientation during scanning of the outer surface of the target region of the mold or crucible. In another embodiment, the system further comprises a robotic apparatus for placing the mold or crucible on the support and for removing the mold or crucible from the support.
[0011] According to another aspect, the present disclosure provides a method for non-destructive evaluation of a mold or crucible. This method involves the steps of: providing a system for non-destructive evaluation according to the present disclosure;
securing a mold or crucible to the support of the system; and operating the 3D scanning device in conjunction with the computer component of the system in order to create a 3D structure difference map that indicates whether the mold or crucible falls within or outside a desired structural integrity parameter range. The 3D structure difference map shows deviations between a 3D
structure generated by scanning an outer surface of a target region of the mold or crucible while secured on the support of the system and a 3D structure of a reference object corresponding to an inner surface of a nominal model of the same target region of the mold or crucible.
In one embodiment, the support of the system further comprises a locating mechanism for positioning the mold or crucible in a repeatable orientation on the support and maintaining the mold or crucible in that orientation during scanning of the outer surface of the target region of the mold or crucible. In another embodiment, the method further involves using a robotic apparatus for placing the mold or crucible on the support and for removing the mold or crucible from the support.
[0012] As provided herein, the present disclosure provides a unique system and a method for measuring the wall thickness of ceramic shell mold and crucible components for use in casting applications. The thickness of the wall of the mold or crucible is important because it has a major effect on the strength of the ceramic shell component. For example, if the thickness of the wall of the ceramic shell component falls below a minimum critical value, the strength of the component falls below the minimum acceptable strength, and the liquid metal can leak from the crucible or mold; the leakage results in a casting failure. If the thickness of the wall of the ceramic shell component falls above a maximum critical value, the component is likely to be improperly located in the casting equipment and require destructive post-processing methods such as external grinding to bring the outer geometry back into specification.
Such a step is a non value-added step in a manufacturing process and would contribute to waste and additional cost. Furthermore, a larger wall thickness may result in providing a larger thermal mass of the shell component, which could result in a change of the melting or solidification dynamics of the casting process.
[0013] Hence, the ability to inspect in a non-destructive manner the thickness of the wall of the ceramic shell component prior to use in the casting application provides the ability to increase casting yields by elimination of the potential failure in the actual casting operation. The NDE capability allows inspection of the full volume of the ceramic component, unlike other techniques, such as sectioning or using coordinate measuring machine (CMM) technologies, which only provide data of a limited portion of the geometry.
[0014] These and other objects, features, and advantages of the systems and methods of the present disclosure will become apparent from the following detailed description of the various aspects of the present disclosure taken in conjunction with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
[0015] FIG. 1 is a schematic of one embodiment of a system for non-destructive evaluation (e.g., wall thickness) of a mold or crucible according to the present disclosure. The schematic shows the basic components of one embodiment, including two laser scanning heads, a central datum reference geometry (i.e., mount portion 24), and the geometry of interest (i.e., crucible 50). In the case of the figure a crucible 50 is shown for the geometry of interest, but this geometry may be of any type. Further, the system may comprise one or a plurality of laser scanning heads to perform the operation. Such details are to be determined by the geometry and quality requirements of the ceramic shell component of interest.
[0016] FIG. 2 is a schematic of one embodiment of a system for non-destructive evaluation (e.g., wall thickness) of a mold or crucible according to the present disclosure. The schematic shows the basic components of the embodiment, including a rigid support frame, two laser scanning heads, a central datum reference geometry (i.e., mount portion 24), and the geometry of interest (i.e., crucible 50). In the case of the figure a crucible 50 is shown for the geometry of interest, but this geometry may be of any type. Further, the system may comprise one or a plurality of laser scanning heads to perform the operation. Such details are to be determined by the geometry and quality requirements of the ceramic shell component of interest.
[0017] FIGS. 3A-3C are illustrations of various aspects of one embodiment of the system of the present disclosure and its use in the non-destructive evaluation of the wall thickness of a crucible. FIG. 3A shows the crucible prior to placement on the fixture of the support of the system of the present disclosure. FIG. 3B shows the fixture and the locating mechanism of the support prior to securing the crucible to the support. FIG.
3C shows the crucible mounted on the fixture and held in place by the locating mechanism of the support.
[0018] FIG. 4 is a flowchart illustrating one embodiment of a method for non-destructive evaluation of a crucible according to the present disclosure.
[0019] FIG. 5 is a flowchart illustrating one embodiment of the step of operating the 3D
scanning device of the system of the present disclosure in conjunction with the computer component in order to determine structural integrity of the crucible.
[0020] FIG. 6 is a flowchart illustrating one embodiment of a method for non-destructive evaluation of a mold according to the present disclosure.
[0021] FIG. 7 is a flowchart illustrating one embodiment of the step of operating the 3D
scanning device of the system of the present disclosure in conjunction with the computer component in order to determine structural integrity of the mold.
[0022] FIGS. 8A-8E are illustrations showing go or no-go dispositions for crucible domes analyzed for wall thickness according to embodiments of the system and method of the present disclosure. These illustrations would be provided by a computer component or printout of results for immediate feedback to the operator.
[0023] FIGS. 9A-9D are illustrations of crucible scans produced in accordance with embodiments of the system and method of the present disclosure showing the repeatability of the scan. This type of inspection shows an example of a calibration routine which would be employed at the start of using the system, and to set initial limits on the repeatability and thus statistical certainty of the measurements.
[0024] FIGS. 10A-10B are images of crucible waxes (also referred to generally as fugitive patterns) used as nominal models for non-destructive evaluation of a crucible using embodiments of a system or method of the present disclosure. The outer surface scan of the crucible wax nominal model can be subtracted from the outer surface scan of a crucible to calculate the wall thickness of the crucible.
[0025] FIG. ibis an image of a wax assembly with two blade waxes (also referred to generally as fugitive patterns) to make a mold with two cavities feed channels and a pour cup to
- 5 -
6 PCT/US2014/037276 cast two blades. The outer surface scan of the wax assembly can be subtracted from the outer surface scan of a mold to calculate the wall thickness of the mold.
[0026] FIGS. 12A-12B are images of crucibles exhibiting an acceptable (FIG.
12A) wall thickness and a rejected (FIG. 12B) wall thickness as determined by embodiments of the system and method of the present disclosure.
[0027] FIGS. 13A-13B are images of crucibles exhibiting a rejected wall thickness as determined by embodiments of the system and method of the present disclosure.
[0028] FIGS. 14A-14C are images of crucibles exhibiting an acceptable (FIG.
14A) wall thickness and a rejected (FIGS. 14B and 14C) wall thickness as determined by embodiments of the system and method of the present disclosure.
[0029] FIG. 15 is a nominal model of a crucible according to one embodiment of the present disclosure. The nominal model can be constructed from point cloud data.
DETAILED DESCRIPTION
[0030] In general, the systems and methods of the present disclosure are effective for the non-destructive evaluation (NDE) of molds and crucibles, such as determining their wall thickness uniformity, conformance to nominal model requirements, and the like.
For example, in certain embodiments, the present disclosure provides a combined electronic and mechanical system that performs surface metrology of shell molds and crucible parts to non-destructively measure wall thickness. Further, the present disclosure provides innovative systems and methods that can be employed to improve casting yield. In a particular embodiment, the system includes: a single or a plurality of three-dimensional (3D) scanning devices (e.g., 3D light or optical scanners) that pass over the shell surface of a crucible; a rigid frame; a fixture that is shaped to the desired internal geometry of the part; and an electronic control, datalogging, and inspection display that provides an operator with the part's disposition (e.g., Accept, Reject, or Rework) based on the laser scanning result, and without destroying or damaging the crucible.
System for Non-Destructive Evaluation of Molds and Crucibles [0031] According to one aspect, the present disclosure provides a system for non-destructive evaluation of a mold or crucible. The system includes a support, a three-dimensional (3D) scanning device, and a computer component. The support comprises a fixture for securing a mold or crucible of interest in place for non-destructive evaluation, with the fixture comprising a mount portion onto which the mold or crucible is secured. The 3D scanning device (e.g., a white light or laser scanner) is effective for scanning an outer surface of a target region of the mold or crucible in order to generate a 3D structure (e.g., a point cloud) of the scanned outer surface of the target region. The computer component is operably connected to the 3D scanning device and effective to create a difference map between the 3D structure of the scanned outer surface of the target region of the mold or crucible and a 3D structure of a reference object corresponding to an inner surface of a nominal model of the same target region of the mold or crucible. The difference map indicates whether the mold or crucible falls within or outside a desired structural integrity parameter range.
[0032] In one embodiment, the 3D scanning device, in operable connection with the computer component, is effective to scan the mount portion of the fixture and/or the fugitive pattern of the mold or crucible in order to generate the 3D structure of the reference object.
[0033] As used herein, the term "nominal model" refers to a computerized 3D
representation of a desired mold or crucible in terms of 3D geometric dimensions. For example, a nominal model is a computerized rendition of the desired mold or crucible that is to be produced. The systems and processes of the present disclosure are suitable for determining whether or not a particular mold or crucible fits the desired nominal model 3D
geometric dimensions.
[0034] As used herein, the term "reference object" refers to any tangible or computerized object that can be used to provide the 3D structure corresponding to the desired inner surface of the nominal model used for creating the difference map with the 3D structure of the scanned outer surface of the target region of the mold or crucible. For example, the reference object can be the mount portion of the fixture of the support of the system of the present disclosure, a fugitive pattern of the mold or crucible, or a computer aided design (CAD) model of the inner surface of a nominal model of the mold or crucible. When the CAD model is the reference object, such CAD model can also be the nominal model as defined herein.
[0035] In certain embodiments, the surface of the mount portion can be scanned with the 3D scanning device to generate 3D structure of the nominal model for the desired inner surface of the crucible or mold. In other embodiments, a fugitive pattern (e.g., a wax or plastic crucible pattern) can be scanned to produce the 3D structure of the nominal model that corresponds to the desired inner surface of the crucible or mold. In addition, the same fugitive pattern may be used in a process for making the crucible or mold according to processes known in the art. In other embodiments, the 3D structure of the nominal model of the desired inner surface of the crucible or mold may be a CAD model.
[0036] As used herein, the term "3D structure" refers to a three-dimensional representation of a scanned structure or a nominal model. For example, the 3D
structure may be
- 7 -in the form of a point cloud, polygonal model or structure, non-uniform rational basis spline (NURBS) surface or structure, and the like.
[0037] As used herein, the "target region" of the mold or crucible refers to a portion or all of the mold or crucible. For example, in some embodiments, the target region can be the dome of the crucible, the sidewalls of the crucible, or the entire crucible (including both the dome and sidewalls of the crucible). In certain embodiments, the target region can be just a portion of the dome of the crucible or a portion of the sidewall of the crucible. In certain embodiments, the target region can be multiple portions of the mold or crucible. For example, the target region can be one or more portions of the dome, one or more portions of the sidewall, or one or more portions of both the dome and sidewall of the crucible.
[0038] As used herein, a "structural integrity parameter" refers to any measurable parameter that can be used to determine the structural integrity of a mold or crucible suitable for use in an investment casting process. For example, as used herein, one example of a structural integrity parameter can include, without limitation, wall thickness of a portion or all of the mold or crucible. More particularly, uniformity of wall thickness of a portion or all of the mold or crucible is an example of a structural integrity parameter as used herein. For certain molds or crucibles, uniformity of wall thickness at particular portions of the mold or crucible may be of more importance than at other portions, as can be determined by one of ordinary skill in the relevant art. In certain embodiments, the structural integrity parameter is effective to determine the amount of stress that the mold or crucible will be able to withstand during a particular investment casting process. For example, in one embodiment, the structural integrity parameter can be one that identifies molds or crucibles that have a yield strength of up to 200 Mega Pascal (MPa). Therefore, the system of the present disclosure is effective for stress management of molds or crucibles used in investment casting processes.
[0039] As used herein, a "desired structural integrity parameter range"
refers to an acceptable range of any measurable parameter that can be used to determine the structural integrity of a mold or crucible suitable for use in an investment casting process, as determined by one of ordinary skill in the art. For example, a desired structural integrity parameter range can be defined by an upper and lower limit of the wall thickness of a portion or all of a mold or crucible. More particularly, the desired structural integrity parameter range can refer to the desired wall thickness of the mold or crucible, or to a percentage of the wall of the mold or crucible that falls within the upper and lower limit of the acceptable range of wall thickness. As provided herein, the desired structural integrity parameter range can be used to determine whether a mold or crucible has an accepted disposition, a rejected disposition, or a rework
- 8 -disposition. Examples of crucibles found to have either an accepted or rejected disposition using the system of the present disclosure are illustrated in the photographs of Figures 12A-12B, 13A-13B, and 14A-14C.
[0040] As used herein, "non-destructive evaluation" (NDE) refers to a process for evaluating a mold or crucible for its structural integrity (e.g., for a particular structural integrity parameter), where the process causes no or substantially no structural or functional damage to the mold or crucible, or where the evaluated mold or crucible may be used for its intended purpose in an investment casting process. As provided herein, the systems and methods of the present disclosure are effective to perform non-destructive evaluation in a manner that measures the full volume geometry of the mold or crucible and/or that measures a desired portion or portions of the mold or crucible.
[0041] In one embodiment, the support of the system further comprises a locating mechanism for positioning the mold or crucible in a repeatable orientation on the support and maintaining the mold or crucible in that orientation during scanning of the outer surface of the target region of the mold or crucible. As used herein, the term "locating mechanism" refers to any mechanical means for directing the placement of the mold or crucible on the support in a desired and repeatable orientation, and for keeping the mold or crucible in that same orientation for NDE purposes in accordance with the present disclosure. For example, in certain embodiments, a series of lugs can be used to define the area of the support where the crucible or mold is to be placed. For example, as shown in Figures 3A and 3C, in a particular embodiment, three lugs 26a and a crucible notch pin 26b can be used to orient and physically maintain the crucible on the support in a desired location and orientation. As shown in Figure 3C, the crucible notch pin 26b fits into the notch 56 of the crucible in order to keep the crucible 50 from twisting or pivoting about the mount portion of the fixture of the support.
[0042] In a particular embodiment, the locating mechanism and the mount portion of the system are configured to work together to position the mold or crucible on the support in a manner that prevents or minimizes damage to the mold or crucible during the non-destructive evaluation. For example, the locating mechanism and mount portion can be configured so that the mold or crucible does not come into physical contact with the support, the locating mechanism, or the mount portion in any way that will damage the structure or function of the mold or crucible during NDE analysis using the system of the present disclosure.
[0043] In one embodiment, the fixture comprises a mount portion having a shape that conforms to an internal surface geometry (also referred to as "datum geometry") of a target region of the mold or crucible. In one embodiment, the mount portion of the fixture of the
- 9 -support has a surface geometry (e.g., 3D surface or surface roughness) and/or surface composition (e.g., materials and coatings used to make the surface of the mount portion) effective to minimize damage to any portion of and in particular the inner surface of the mold or crucible during mounting, maintaining, and/or removing of the mold or crucible to or from the support. In certain embodiments, the mount portion of the fixture can be made of or coated with a material that is known to minimize damage to the internal surface of the mold or crucible.
Minimizing damage includes, for example, ensuring that no or substantially no marks, nicks, scratches, or the like are left behind on the locating surface of the ceramic geometry of the mold or crucible after undergoing NDE processing using a system and/or method according to the present disclosure. For certain investment casting applications, such marks, nicks, scratches, or the like of the mold or crucible may be considered as defects requiring the discarding of the part when they are larger than a particular size when measured in any dimension (e.g., larger than 0.5 mm in size as measured by length, width, and/or depth). Materials can be chosen to further reduce the size of potential defects to a more preferred specification (e.g., of less than 0.100 microns). In a particular embodiment, the act of securing and removing the mold or crucible (e.g., a ceramic shape) to the internal reference datum geometry (e.g., the mount portion of the fixture) should result in defects less than 50 microns in size. Suitable examples of materials for use in making the mount portion of the fixture can include, without limitation, silicone coatings, natural rubbers, acrylic paint coatings, plastic materials, and/or smoothly-polished metals.
[0044] In one embodiment of the system of the present disclosure, the 3D
scanning device is fixed or not fixed to the support. In another embodiment of the system of the present disclosure, the 3D scanning device is operably connected to a robotic system for maneuvering the 3D scanning device during the scanning of the outer surface of the target region, or during scanning of the surface of the reference object. The 3D scanning device can include one or more 3D scanning heads. Further, the 3D scanning device can be any device effective to scan a surface in order to create a corresponding point cloud, polygonal structure, or non-uniform rational basis spline (NURBS) structure of that surface, which can be, without limitation, the outer surface of the target region of the mold or crucible or the surface of a reference object as used herein.
[0045] In various embodiments of the present disclosure, the 3D scanning device can operate in accordance with many different approaches for short-range, non-contact 3D scanning techniques. As is known by those of ordinary skill in the relevant art, a 3D
scanner collects distance information about surfaces within its field-of-view (FOY).
- 10 -[0046] There are three broad categories of 3D scanning techniques, namely, triangulation, structured light, and time-of-flight. Triangulation typically emits a laser light to determine the shape and position of the object. An offset camera is used to detect the reflected light. Geometry is used to calculate the distances. The baseline between the camera and the laser is known, and so is the angle of the laser. Structured light or white light 3D scanners also use triangulation. However, instead of using a laser it projects a pattern on the object. The whole FOV is captured at once, but several different patterns are projected in sequence over . time. Each pixel in the camera will have a 3D location associated with it. Time-of-flight is typically used for larger objects. It uses a laser range finder and a means of moving the azimuth/elevation of the laser point. A pulse of light is timed to measure the distance to the object. When combined with the azimuth and elevation, it gives you the 3D
location of the point. The laser it typically scanned with rotating mirrors to create a dense 3D point cloud.
[0047] The 3D scanning device of the present disclosure can include any scanning device effective for 3D scanning using triangulation, structure light (e.g., white light), and time-of-flight 3D scanning techniques. Thus, the 3D scanning device can include a structured light scanner (e.g., a white light scanner), a laser scanning device (e.g., laser scanner), or any other device effective for performing the 3D scanning techniques according to the present disclosure.
[00481 As provided herein, the 3D scanning device may be a laser scanning device. The laser scanning device can include, without limitation, a laser scanning head effective to generate a three-dimensional structure (e.g., a point cloud) of a scanned surface. In one embodiment, the laser scanning head can include, without limitation, a laser transceiver and a two-axis oscillating mirror. The laser scanning device can include a single laser scanning head or a plurality of laser scanning heads. Suitable examples of laser scanning devices for use in the system can include, without limitation, laser scanning devices made or sold by Konica MinoltaTM
(VIVID scanner), threeRiversTM 3D (Virtuoso scanner), Shape DriveTM (3D scanner), and the like.
Those of ordinary skill in the art can readily determine other 3D scanning devices and 3D laser scanners for use in the system of the present disclosure.
100491 As used herein, a suitable computer component can include any computer system (e.g., computer, software, peripherals, etc.) that can run the 3D scanning device and provide an output disposition with respect to a mold or crucible that has undergone an NDE process using the system or method of the present disclosure. Suitable computer components and computer systems for use in the systems and methods of the present disclosure are known by those of ordinary skill in the art.
-Il-[0050] In one embodiment, the computer component comprises a computer and software that, in an automated fashion, sends operation signals to the 3D scanning device, receives scanning data from the 3D scanning device, compares the received scanning data to desired mold or crucible specifications, and displays a disposition as to whether the mold or crucible has measurements that fall within or outside the desired structural integrity parameter range of the non-destructive evaluation, wherein the desired structural integrity parameter comprises measurement of full volume geometry or wall thickness of the mold or crucible.
In a particular embodiment, the disposition provided by the computer component identifies the wall thickness as being either within or outside of the specification limits, thereby displaying whether the wall thickness has an accepted disposition or a rejected disposition.
100511 In one embodiment, the computer component captures dimensions and tolerances specific to wall thickness, circularity, concentricity, and/or parallelism of the region of the mold or crucible undergoing NDE.
[0052] In another embodiment, the system further comprises a robotic apparatus for placing the mold or crucible on the support and for removing the mold or crucible from the support. In a particular embodiment, the robotic apparatus is effective to remove the non-destructively evaluated molds or 'crucibles from the support and segregate them into their respective collection areas according to whether they are identified as accepted (e.g., pass), rejected (e.g., fail), or rework dispositions. Suitable robotic apparatuses for use in the system of the present disclosure arc known by those of ordinary skill in the art.
Examples of suitable robotic apparatuses can include those manufactured or sold by Kuka Industrial RobotsTM, Adept Technology, Inc.TM, Staubli RoboticsTM, ABB RoboticsTM, etc.
100531 Illustrative examples of systems of the present disclosure are provided in Figure 1 and Figure 2, which are schematic diagrams of various embodiments of system 10 for non-destructive evaluation of a mold or crucible 50. As shown in Figures 1 and 2, system 10 includes a support 20, a 3D scanning device 30, and a computer component 40.
Support 20 comprises a fixture 22 for securing a mold or crucible 50 of interest in place for non-destructive evaluation of mold or crucible 50. Fixture 22 comprises a mount portion 24 onto which mold or crucible 50 is secured. In certain embodiments, mount portion 24 has a shape that conforms to an internal surface geometry of a target region 52 of mold or crucible 50.
Support 20 may further include locating mechanism 26 for positioning mold or crucible 50 in a repeatable orientation on support 20 and maintaining mold or crucible 50 in that orientation during scanning of outer surface 54 of target region 52 of mold or crucible 50. 3D
scanning device 30 is used for scanning an outer surface 54 of target region 52 of mold or crucible 50 in order to generate a 3D structure (e.g., a point cloud) of scanned outer surface 54 of target region 52 of mold or crucible 50. The 3D scanning device may be fixed to the support (see Figure 2) or may be independent from the support (see Figure 1). The 3D scanning device may be a laser scanning device and include a single laser scanning head or a plurality of laser scanning heads.
Computer component 40 is operably connected to 3D scanning device 30 and effective to create a difference map between the 3D structure (e.g., point cloud) of the scanned outer surface 54 of the target region 52 of mold or crucible 50 and the 3D structure of a reference object (e.g., a point cloud thereof) corresponding to an inner surface of a nominal model of the same target region of mold or crucible 50. The difference map indicates whether the mold or crucible falls within or outside a desired structural integrity parameter range.
[0054] Figures 3A, 3B, and 3C are photographic images of one embodiment of system 10. In particular, Figures 3A, 3B, and 3C illustrate one embodiment of locating mechanism 26 (denoted as 26a and 26b) for positioning mold or crucible 50 in a repeatable orientation on support 20 and maintaining mold or crucible 50 in that orientation during scanning of the outer surface of the target region of mold or crucible 50, and more particularly for positioning mold or crucible 50 on mount portion 24. Figure 3A shows crucible 50 prior to being secured to mount portion 24 of system 10. Crucible 50 is shown to include notch 56 (also referred to as a groove or door). Figure 3B shows system 10 having mount portion 24 of fixture 22 and locating mechanism 26, with the locating mechanism being shown more particularly as locating mechanism lugs 26a and locating mechanism crucible notch pin 26b. Figure 3C
shows crucible 50 securely mounted on mount portion 24 and secured in place by locating mechanism 26, where locating mechanism lugs 26a orient the placed crucible 50 in the desired location and locating mechanism crucible notch pin 26b fits into crucible notch 56 in a manner that is effective to keep crucible 50 from rotating about the mount portion during NDE
analysis. While three locating mechanism lugs are shown in Figures 3B, the present disclosure is not limited to any particular number of such lugs. Thus, the present disclosure contemplates any mechanical means that can be used to orient and maintain the mold or crucible in a desired orientation and position on the support during NDE analysis according to the systems and methods of the present disclosure.
Method for Non-Destructive Evaluation of Molds and Crucibles [0055] According to another aspect, the present disclosure provides a method for non-destructive evaluation of a mold or crucible. This method involves the steps of: providing a system for non-destructive evaluation according to the present disclosure;
securing a mold or crucible to the support of the system; and operating the three-dimensional (3D) scanning device of the system in conjunction with the computer component of the system in order to create a 3D
structure (e.g., a point cloud) difference map that indicates whether the mold or crucible falls within or outside a desired structural integrity parameter range. The 3D
structure (e.g., point cloud) difference map shows deviations between a 3D structure (e.g., point cloud) generated by scanning an outer surface of a target region of the mold or crucible while secured on the support of the system and a 3D structure (e.g., point cloud) of a reference object corresponding to an inner surface of a nominal model of the same target region of the mold or crucible.
[0056] With regard to this method, the system for use in this method is as described in the present disclosure.
[0057] According to one embodiment of the method of the present disclosure, the mold or crucible is determined to have either: (i) an acceptable disposition if at least between about 75 and about 90 percent of the difference map falls within the desired structural integrity parameter range; (ii) a rejected disposition if more than between about 10 and about 25 percent of the difference map falls below the desired structural parameter range; or (iii) a rework disposition if more than between about 10 and about 25 percent of the difference map falls above the desired structural parameter range.
[0058] As noted herein, the method can involve using the system of the present disclosure to determine whether the mold or crucible falls within or outside of a desired structural integrity parameter, e.g., wall thickness of a portion or all of the mold or crucible. The method can be used for non-destructive evaluation that involves measuring full volume geometry of the mold or crucible. As an illustrative example, the desired structural integrity parameter can be wall thickness of the dome of a crucible, where the wall thickness is desired to be within a particular thickness range in millimeters. If the crucible is found to fall within the desired thickness range, then it is determined to have an accepted disposition, and therefore can be used as is. If the crucible is found to fall below the desired thickness range, then it is determined to have a rejected disposition because it is too thin for its intended purpose (e.g., investment casting processes), and therefore should be discarded and not used.
If the crucible is found to fall above the desired thickness range, then it is determined either to have a rejected disposition or a rework disposition. A rework disposition can mean that, while a portion of the crucible may be too thick, that portion could be reworked (e.g., ground) to bring it within the desired thickness range.

[0059] In certain embodiments, the method uses a structural integrity parameter that is effective to determine the amount of stress that the mold or crucible will be able to withstand during a particular investment casting process. For example, in one embodiment, the structural integrity parameter can be one that identifies molds or crucibles that have a yield strength of up to 200 Mega Pascal (MPa). Therefore, the system of the present disclosure is effective for stress management of molds or crucibles used in investment casting processes.
[0060] In one embodiment, the nominal model can be generated using algorithms for surface modeling based on the point cloud data, or derived from 3D solid models based on engineering specifications. An example of a nominal model in accordance with the present disclosure is shown in Figure 15.
[0061] In various embodiments, the method involves operating the computer component's control software in order to calculate the wall thickness of the mold or crucible using the reference datum geometry scan, nominal model, and actual geometry point cloud data.
[0062] In one embodiment, the support of the system further comprises a locating mechanism for positioning the mold or crucible in a repeatable orientation on the support and maintaining the mold or crucible in that orientation during scanning of the outer surface of the target region of the mold or crucible. In various embodiments, the mount portion of the fixture can have a surface geometry and/or surface composition effective to prevent or minimize damage to the inner surface of the mold or crucible during mounting, maintaining, and/or removing the mold or crucible to or from the support.
[0063] In one embodiment, the step of securing the mold or crucible to the support of the system comprises: (i) providing a support whose locating mechanism and mount portion are configured to work together to position the mold or crucible on the support in a manner that prevents or minimizes damage to the mold or crucible during the non-destructive evaluation; and (ii) securing the mold or crucible in place on the support so that the inner surface of the mold or crucible has a desired contact with the mount portion of the fixture. In a particular embodiment, the desired contact is based on location of contact and amount of contact, wherein the amount of contact ranges from no contact to full contact with the mount portion of the fixture.
100641 In one embodiment of the method of the present disclosure, the step of operating the 3D scanning device in conjunction with the computer component comprises using the computer component to execute the following steps in an automated fashion, the steps comprising: (i) sending operation signals to the 3D scanning device; (ii) receiving scanning data from the 3D scanning device; (iii) comparing the received scanning data to desired mold or crucible specifications; and (iv) displaying a disposition as to whether the mold or crucible has measurements that fall within or outside the desired structural integrity parameter of the non-destructive evaluation, wherein the desired structural integrity parameter comprises measurement of full volume geometry or wall thickness of the mold or crucible.
[0065] In one embodiment, the step of sending operation signals to the 3D
scanning device comprises: (i) directing the 3D scanning device to scan the surface of the reference object to produce the initial datum geometry reference scan prior to securing the mold or crucible in place on the support; (ii) directing the 3D scanning device to scan the outer surface of the target region of the mold or crucible to generate a corresponding 3D
structure (e.g., point cloud) of the target region; or (iii) directing the 3D scanning device to scan the surface of the reference object to produce the initial datum geometry reference scan prior to securing the mold or crucible in place on the support, and thereafter to scan the outer surface of the target region of the mold or crucible to generate the corresponding 3D structure (e.g., point cloud) when the mold or crucible is in place on the support.
[0066] In one embodiment, the method involves performing best-fit and other mathematical calculations using a 3D nominal CAD model to orient the scanning data. In one embodiment, the disposition provided by the computer component identifies the full volume geometry and/or the wall thickness of the mold or crucible as being either within or outside of the specification limits, thereby displaying whether the full volume geometry or wall thickness of the mold or crucible has an accepted disposition, a rejected disposition, or a rework disposition.
[0067] In one embodiment, the step of operating the 3D scanning device in conjunction with the computer component of the system in order to create the 3D structure difference map comprises the following steps: using the 3D scanning device of the system or a different 3D
scanning device to scan the surface of the reference object to generate the 3D
structure of the reference object; using the 3D scanning device of the system to scan the outer surface of the target region of the mold or crucible to generate the 3D structure of said target region; and using the computer component to create the 3D structure difference map to determine whether the mold or crucible fails within or outside of the desired structural integrity parameter range. In a particular embodiment, the reference object comprises either the mount portion of the fixture or a fugitive pattern of the mold or crucible (e.g., a wax mold or crucible).
[0068] In one embodiment, the step of operating the 3D scanning device in conjunction with the computer component of the system in order to create the 3D structure difference map comprises the following steps: providing a computer aided design (CAD) model of the inner surface of a nominal model of the mold or crucible; using the 3D scanning device of the system to scan the outer surface of the target region of the mold or crucible to generate the 3D structure of said target region; and using the computer component to create the 3D
structure difference map to determine whether the mold or crucible fails within or outside of the desired structural integrity parameter range.
[0069] In one embodiment, the method is performed on a plurality of different molds or crucibles using the same 3D structure of the reference object.
[0070] In another embodiment, the method further involves using a robotic apparatus for placing the mold or crucible on the support and for removing the mold or crucible from the support. In certain embodiments, the robotic apparatus is programmed to automatically place the molds or crucibles into segregated locations according to their dispositions as either accepted, rejected, or rework, after having undergone NDE analysis according to the method of the present disclosure.
[0071] Figure 4 and Figure 5 illustrate embodiments of various aspects of the methods of the present disclosure for non-destructive evaluation of a crucible.
[0072] Figure 4 is a flowchart illustrating one embodiment of method 100 for non-destructive evaluation of a crucible. As shown in Figure 4, method 100 includes the steps of:
providing a system for non-destructive evaluation of a crucible according to the present disclosure (step 110); securing a crucible to the support of the system (step 120); and operating the 3D scanning device of the system in conjunction with the computer component of the system in order to create a 3D structure (e.g., point cloud) difference map that indicates whether the crucible falls within or outside a desired structural integrity parameter range (step 130). In order to position the crucible in a repeatable orientation on the support, the support can include a locating mechanism as described herein. As discussed previously, the system of the present disclosure that is used in this method is effective to measure full volume wall thickness of the crucible.
[0073] As shown in the flowchart of Figure 5, in one embodiment of method 100, operating the 3D scanning device with the computer component (step 130) comprises the following: sending operation signals to the 3D scanning device (step 131);
receiving scanning data from the 3D scanning device (step 132); comparing the received scanning data to desired crucible specifications (step 133); and displaying a disposition as to whether the crucible has measurements that fall within or outside the desired structural integity parameter of the non-destructive evaluation (step 134), wherein the desired structural integrity parameter comprises measurement of full volume geometry or wall thickness of the crucible.

[0074] Figure 6 and Figure 7 illustrate embodiments of various aspects of the methods of the present disclosure for non-destructive evaluation of a mold. In these embodiments, a wax is used to establish the inner surface geometry of the desired mold.
[0075] Figure 6 is a flowchart illustrating one embodiment of method 200 for non-destructive evaluation of a mold. As shown in Figure 6, method 200 includes:
providing a system for non-destructive evaluation of a mold according to the present disclosure (step 210);
securing a mold to the support of the system (step 220); and operating the 3D
scanning device of the system in conjunction with the computer component of the system in order to create a 3D
structure (e.g., point cloud) difference map that indicates whether the mold falls within or outside a desired structural integrity parameter range (step 230). In order to position the mold in a repeatable orientation on the support, the support can include a locating mechanism as described herein. As discussed previously, the system of the present disclosure that is used in this method is effective to measure full volume wall thickness of the mold.
[0076] As shown in the flowchart of Figure 7, in one embodiment of method 200, operating the 3D scanning device with the computer component (step 230) comprises the following: sending operation signals to the 3D scanning device (step 231);
receiving scanning data from the 3D scanning device (step 232); comparing the received scanning data to desired mold specifications (step 233); and displaying a disposition as to whether the mold has measurements that fall within or outside the desired structural integity parameter of the non-destructive evaluation (step 234), wherein the desired structural integrity parameter comprises measurement of full volume geometry or wall thickness of the mold.
[0077] In one embodiment of the method of the present disclosure, the disposition provided by the computer component identifies the wall thickness as being either within or outside of the specification limits, thereby displaying whether the wall thickness has an accepted disposition or a rejected disposition.
[0078] In one embodiment of the method of the present disclosure, the computer component captures dimensions and tolerances specific to wall thickness, circularity, conccntricity, and/or parallelism of the region of thc mold or crucible.
EXAMPLES
[0079] The following examples are intended to illustrate particular embodiments, but are by no means intended to limit the scope of the present systems and techniques.
Example 1 [0080] In one embodiment, the system of the present disclosure includes one or a plurality of laser scanning heads, a rigid frame stand to hold the scanning head which may include mechatronic motion of the scanning head, a fixture to locate the inspected part, and an inspection logging and decisioning computer. The laser scanning head works by means of a typical commercial off-the-shelf scanning head, which consists of a laser transceiver and a two-axis oscillating mirror. When mapped over polar positions of the mirror by governing software, a point cloud is generated which corresponds to a mapping of the measured surface. Multiple laser scanning heads may be employed to increase the point density and thus accuracy of the measurement. The inspection and logging decisioning computer includes a control computer and software that sends operation signals to the scanning unit, receives scanning data from the unit, compares the data to part specifications, and displays a disposition in an automated fashion. The computer may be PC-based or any other simple computing machine. The software compares the point cloud of the measured external surface and creates a difference map between the measured external surface point cloud and a known nominal shape (in the software's 3D
space) representing the geometry of the crucible, and specifically the internal geometry of the dome of the crucible. The difference map provides a mapping of the crucible wall thickness of the dome of the crucible.
[0081] As shown in Figures 8A-8E, thickness acceptability is represented as a 3D
surface map wherein the surfaces are color-coded or otherwise marked based on disposition.
For example, as shown in Figures 8A-8E, an accepted wall thickness can shown in green (denoted as reference number 42 in Figures 8A-8E), a rejected wall thickness can be shown in red (denoted as reference number 44 in Figures 8A, 8B, 8C, and 8E), and a rework wall thickness (i.e., greater thickness than accepted thicknesses) can be shown in blue (not shown in the figures). Thus, when the wall thickness is below lower specification limits, the software shows the surface in color-coded red (shown in Figures 8A, 8B, 8C, and 8E as reference numbers 44) to denote that the thickness is below minimum specifications. If the thickness is above maximum limits, the surface is color-coded blue to denote that a rework operation is needed. To determine overall part disposition, a threshold minimum surface area is chosen.
Typically this figure is 20 percent for regions of the crucible that are not highly stressed during melting. This means that if more than 20 percent of the measured surface area is below minimum thickness, the software triggers a Reject disposition. If more than this threshold percentage (or another threshold percentage for upper limits) is above maximum thickness, a Rework disposition is reported. Otherwise, an Accept disposition is reported.

[0082] The rigid fixture consists of a smooth geometry that closely fits the internal geometry of the dome of the inspected crucible, and is of a shape, surface finish, and hardness that is selected to ensure minimum damage of the internal surface of the dome of the crucible during the measurement operation. The geometry of the dome of the crucible may be ball or spheroidal-shaped, or any other shape appropriate to fit tightly into the dome of the crucible part without damage. To further minimize damage to the internal surface, the spheroidal insert may be coated with paint, polymer coating, a high durometer rubber, or similar soft material. The fixture also consists of locating geometry to ensure the crucible part is oriented in a repeatable position (see Figures 9A-9D). Figures 9A-9D show different scans of the same crucible where the crucible is removed and reinstalled and then scanned/rescanned. As shown in Figures 9A-9D, the scans are virtually identical.
[0083] The frame includes mechanical pieces including structural members and a table (steel or granite) to hold the laser scanning head in a precise fixed position from the fixture, with optional provisions for vibration reduction. Linear motion components such as ball screws and servo motors may be included to provide precise positioning of the laser scanning head(s).
Example 2 [0084] In a second embodiment, the system of the present disclosure includes one or a plurality of laser scanning heads, a rigid frame stand to hold the scanning head which may include mechatronic motion of the scanning head, a fixture to locate the inspected part, and an inspection logging and decisioning computer. The laser scanning head works by means of a typical commercial off-the-shelf scanning head, which consists of a laser transceiver and a two-axis oscillating mirror, as described in the previous example. When mapped over polar positions of the mirror by governing software, a point cloud is generated which corresponds to a mapping of the measured surface. Multiple laser scanning heads may be employed to increase the point density and thus accuracy of the measurement. In this example the system is used to measure the wall thickness of both the dome section and the straight wall sections of the crucible. A wax pattern is uscd to measurc a point cloud of the intcrnal surface of both the dome section and the straight wall sections of the crucible. A 3-D surface model is then generated of the external surface of the crucible, and this model is then used as a representation of the internal surface of resulting crucible. Photographs of a suitable crucible wax patterns are shown in Figures 10A-10B. The same wax pattern, or an equivalent wax pattern, is used to produce the crucible by a previously disclosed slurry-dip process, or a similar process.

[0085] The inspection and logging decisioning computer includes a control computer and software that sends operation signals to the scanning unit, receives scanning data from the unit, compares the data to part specifications, and displays a disposition in an automated fashion.
The computer may be PC-based or any other simple computing machine. The software compares the point cloud of the measured external surface against the model that was generated of the external surface of the wax, which is used as a representation of the internal surface of the resulting crucible and a difference map is generated between the measured external surface point cloud and the model of the internal surface of the crucible. The difference map corresponds to a mapping of the crucible wall thickness in the dome of the crucible.
[0086] When the wall thickness is below lower specification limits, the software triggers a Reject disposition. If the thickness is within upper and lower specification limits, the software triggers an Accept disposition. If the thickness is above the upper specification limit, a Rework disposition is reported. The fixture also consists of locating geometry to ensure the crucible part is oriented in a repeatable position.
Example 3 [0087] In a third embodiment, the system of the present disclosure includes one or a plurality of laser scanning heads, a rigid frame stand to hold the scanning head which may include mechatronic motion of the scanning head, a fixture to locate the inspected part, and an inspection logging and decisioning computer. The laser scanning head works by means of a typical commercial off-the-shelf scanning head, which consists of a laser transceiver and a two-axis oscillating mirror, as described in the previous example. In this example the system is used to measure the wall thickness of a mold. The starting point for determining the mold wall thickness is the wax pattern assembly that is used to generate the mold. The laser scanner, as described in the previous examples, is used to generate a point cloud which corresponds to an initial mapping of the measured external surface of the wax pattern.
Subsequently, a point cloud is generated which corresponds to a mapping of the measured external surface of the mold built from thc wax pattern. Multiple laser scanning heads may be employed to increase the point density and thus accuracy of the measurement. A 3-D surface model is generated from the point cloud of the external surface of the mold wax assembly, and this surface model is then used as a representation of the internal surface of the resulting mold wax assembly.
Photographs of a typical wax pattern assembly used to make a mold is shown in Figure 11. The same wax pattern, or an equivalent wax pattern, is used to produce the mold by a previously disclosed slurry-dip process, or a similar process.

[0088] The inspection and logging decisioning computer includes a control computer and software that sends operation signals to the scanning unit, receives scanning data from the unit, compares the data to part specifications, and displays a disposition in an automated fashion.
The computer may be PC-based or any other simple computing machine. The software compares the point cloud of the measured external surface of the mold against the 3-D surface model that was generated from the external surface of the wax, which is used as a representation of the internal surface of the resulting mold, and a difference map is generated between the measured external surface point cloud and the model of the internal surface of the mold. The difference map corresponds to a mapping of the mold wall thickness.
[0089] When the wall thickness is below lower specification limits, the software triggers a Reject disposition. If the wall thickness of the mold is within upper and lower specification limits, the software triggers an Accept disposition. If the thickness is below the lower specification limit or above the upper specification limit, the mold is rejected because it will not make a satisfactory component. For example, if the mold is too thin, it can break during casting and cause a mold leak and casting failure. If the mold is too thick, it can cause cracking of the part during post solidification cool down due to differential thermal expansion mismatch between the mold and component. The fixture can contain a locating geometry to ensure the mold part is oriented in a repeatable position.
[0090] Although various embodiments have been depicted and described in detail herein, it will be apparent to those skilled in the relevant art that various modifications, additions, substitutions, and the like can be made without departing from the scope of the invention and these are therefore considered to be within the scope of the invention as defined in the claims which follow.

Claims (43)

WHAT IS CLAIMED IS:
1. A system for non-destructive evaluation of a mold or crucible, said system comprising:
a support comprising a fixture for securing a ceramic or refractory oxide mold or crucible in place for non-destructive evaluation, said fixture comprising a mount portion onto which the ceramic or refractory oxide mold or crucible is secured;
a three-dimensional (3D) scanning device for scanning an outer surface of a target region of the ceramic or refractory oxide mold or crucible in order to generate a 3D structure of the scanned outer surface of the target region; and a computer component operably connected to the 3D scanning device and effective to create a difference map between the 3D structure of the scanned outer surface of the target region of the ceramic or refractory oxide mold or crucible and a 3D structure of a reference object corresponding to an inner surface of a nominal model of the same target region of the ceramic or refractory oxide mold or crucible, wherein said difference map indicates whether the ceramic or refractory oxide mold or crucible falls within or outside a desired structural integrity parameter range.
2. The system according to claim 1, wherein the reference object comprises either the mount portion of the fixture or a fugitive pattern of the ceramic or refractory oxide mold or crucible.
3. The system according to claim 2, wherein the 3D scanning device, in operable connection with the computer component, is effective to scan the mount portion of the fixture and/or the fugitive pattern of the ceramic or refractory oxide mold or crucible in order to generate the 3D structure of the reference object.
4. The system according to claim 1, wherein the inner surface of the nominal model of the ceramic or refractory oxide mold or crucible comprises a computer aided design (CAD) model thereof.
5. The system according to claim 1, wherein the target region is a portion or all of the ceramic or refractory oxide mold or crucible.
6. The system according to claim 1, wherein the desired structural integrity parameter comprises wall thickness of a portion or all of the ceramic or refractory oxide mold or crucible.
7. The system according to claim 1, wherein the non-destructive evaluation comprises measuring full volume geometry of the ceramic or refractory oxide mold or crucible.
8. The system according to claim 1, wherein the support further comprises a locating mechanism for positioning the ceramic or refractory oxide mold or crucible in a repeatable orientation on the support and maintaining the ceramic or refractory oxide mold or crucible in that orientation during scanning of the outer surface of the target region of the ceramic or refractory oxide mold or crucible.
9. The system according to claim 8, wherein the locating mechanism and the mount portion are configured to work together to position the ceramic or refractory oxide mold or crucible on the support in a manner that prevents or minimizes damage to the ceramic or refractory oxide mold or crucible during the non-destructive evaluation.
10. The system according to claim 1, wherein the mount portion of the fixture has a surface geometry and/or surface composition effective to minimize damage to the inner surface of the ceramic or refractory oxide mold or crucible during mounting, maintaining, and/or removing the ceramic or refractory oxide mold or crucible to or from the support.
11. The system according to claim 1, wherein the 3D scanning device is fixed or not fixed to the support.
12. The system according to claim 1, wherein the 3D scanning device is operably connected to a robotic system for maneuvering the 3D scanning device during the scanning of the outer surface of the target region.
13. The system according to claim 1, wherein the 3D scanning device is effective to scan the outer surface of the target region in order to create a corresponding point cloud, polygonal structure, or non-uniform rational basis spline (NURBS) structure of the outer surface of the target region.
14. The system according to claim 1, wherein the 3D scanning device is selected from the group consisting of a white light scanner and a laser scanning device.
15. The system according to claim 14, wherein the laser scanning device comprises a laser scanning head effective to generate a three-dimensional point cloud of a scanned surface.
16. The system according to claim 15, wherein the laser scanning device comprises a single laser scanning head or a plurality of laser scanning heads.
17. The system according to claim 1, wherein the computer component comprises a computer and software that, in an automated fashion, sends operation signals to the 3D scanning device, receives scanning data from the 3D scanning device, compares the received scanning data to desired mold or crucible specifications, and displays a disposition as to whether the mold or crucible has measurements that fall within or outside the desired structural integrity parameter range of the non-destructive evaluation, wherein the desired structural integrity parameter comprises measurement of full volume geometry or wall thickness of the ceramic or refractory oxide mold or crucible.
18. The system according to claim 1, wherein the computer component captures dimensions and tolerances specific to wall thickness, circularity, concentricity, and/or parallelism of the region of the ceramic or refractory oxide mold or crucible.
19. The system according to claim 1 further comprising:
a robotic apparatus for placing the ceramic or refractory oxide mold or crucible on the support and for removing the ceramic or refractory oxide mold or crucible from the support.
20. A method for non-destructive evaluation of a mold or crucible, said method comprising:
providing a system for non-destructive evaluation according to claim 1;
securing the ceramic or refractory oxide mold or crucible to the support of the system; and operating the three-dimensional (3D) scanning device in conjunction with the computer component of the system in order to create a 3D structure difference map that indicates whether the ceramic or refractory oxide mold or crucible falls within or outside a desired structural integrity parameter range, wherein the 3D structure difference map shows deviations between a 3D
structure generated by scanning an outer surface of a target region of the ceramic or refractory oxide mold or crucible while secured on the support of the system and a 3D
structure of a reference object corresponding to an inner surface of a nominal model of the same target region of the ceramic or refractory oxide mold or crucible.
21. The method according to claim 20, wherein the target region is a portion or all of the ceramic or refractory oxide mold or crucible.
22. A method for non-destructive evaluation of a mold or crucible, said method comprising:
providing a system for non-destructive evaluation comprising:
a support comprising a fixture for securing a ceramic or refractory oxide mold or crucible in place for non-destructive evaluation, said fixture comprising a mount portion onto which the ceramic or refractory oxide mold or crucible is secured;
a three-dimensional (3D) scanning device for scanning an outer surface of a target region of the ceramic or refractory oxide mold or crucible in order to generate a 3D structure of the scanned outer surface of the target region;
and a computer component operably connected to the 3D scanning device and effective to create a difference map between the 3D structure of the scanned outer surface of the target region of the ceramic or refractory oxide mold or crucible and a 3D structure of a reference object corresponding to an inner surface of a nominal model of the same target region of the ceramic or refractory oxide mold or crucible, wherein said difference map indicates whether the ceramic or refractory oxide mold or crucible falls within or outside a desired structural integrity parameter range;
securing the mold or crucible to the support of the system; and operating the three-dimensional (3D) scanning device in conjunction with the computer component of the system in order to create a 3D structure difference map that indicates whether the mold or crucible falls within or outside a desired structural integrity parameter range, wherein the 3D structure difference map shows deviations between a 3D
structure generated by scanning an outer surface of a target region of the mold or crucible while secured on the support of the system and a 3D structure of a reference object corresponding to an inner surface of a nominal model of the same target region of the mold or crucible, wherein the mold or crucible is determined to have either:
an acceptable disposition if at least between about 75 and about 90 percent of the difference map falls within the desired structural integrity parameter range, a rejected disposition if more than between about 10 and about 25 percent of the difference map falls below the desired structural parameter range; or a rework disposition if more than between about 10 and about 25 percent of the difference map falls above the desired structural parameter range.
23. The method according to claim 20, wherein the desired structural integrity parameter comprises wall thickness of a portion or all of the ceramic or refractory oxide mold or crucible.
24. The method according to claim 20, wherein the method of non-destructive evaluation comprises measuring full volume geometry of the ceramic or refractory oxide mold or crucible.
25. The method according to claim 20, wherein the nominal model is generated using algorithms for surface modeling based on point cloud data, or derived from 3D solid models based on engineering specifications.
26. The method according to claim 20, wherein the support of the system further comprises a locating mechanism for positioning the ceramic or refractory oxide mold or crucible in a repeatable orientation on the support and maintaining the ceramic or refractory oxide mold or crucible in that orientation during scanning of the outer surface of the target region of the ceramic or refractory oxide mold or crucible.
27. The method according to claim 26, wherein securing the mold or crucible to the support of the system comprises:
providing a support whose locating mechanism and mount portion are configured to work together to position the ceramic or refractory oxide mold or crucible on the support in a manner that prevents or minimizes damage to the ceramic or refractory oxide mold or crucible during the non-destructive evaluation;
and securing the ceramic or refractory oxide mold or crucible in place on the support so that the inner surface of the ceramic or refractory oxide mold or crucible has a desired contact with the mount portion of the fixture.
28. The method according to claim 27, wherein the desired contact is based on location of contact and amount of contact, wherein the amount of contact ranges from no contact to full contact with the mount portion of the fixture.
29. The method according to claim 20, wherein the mount portion of the fixture has a surface geometry and/or surface composition effective to prevent or minimize damage to the inner surface of the ceramic or refractory oxide mold or crucible during mounting, maintaining, and/or removing the ceramic or refractory oxide mold or crucible to or from the support.
30. The method according to claim 20, wherein the 3D scanning device is fixed or not fixed to the support.
31. The method according to claim 20, wherein the 3D scanning device is operably connected to a robotic system for maneuvering the 3D scanning device during the scanning of the outer surface of the target region.
32. The method according to claim 20, wherein the 3D scanning device is effective to scan the outer surface of the target region in order to create a corresponding point cloud, polygonal structure, or non-uniform rational basis spline (NURBS) structure of the outer surface of the target region.
33. The method according to claim 20, wherein the 3D scanning device is selected from the group consisting of a white light scanner and a laser scanning device.
34. The method according to claim 33, wherein the laser scanning device comprises a laser scanning head effective to generate a three-dimensional point cloud of a scanned surface.
35. The method according to claim 34, wherein the laser scanning device comprises a single laser scanning head or a plurality of laser scanning heads.
36. The method according to claim 20, wherein the computer component captures dimensions and tolerances specific to wall thickness, circularity, concentricity, and/or parallelism of the region of the ceramic or refractory oxide mold or crucible.
37. The method according to claim 20, wherein operating the 3D
scanning device in conjunction with the computer component comprises using the computer component to execute in an automated fashion:
sending operation signals to the 3D scanning device;
receiving scanning data from the 3D scanning device;
comparing the received scanning data to desired ceramic or refractory oxide mold or crucible specifications; and displaying a disposition as to whether the ceramic or refractory oxide mold or crucible has measurements that fall within or outside the desired structural integrity parameter of the non-destructive evaluation, wherein the desired structural integrity parameter comprises measurement of full volume geometry or wall thickness of the ceramic or refractory oxide mold or crucible.
38. The method according to claim 37, wherein sending operation signals to the 3D scanning device comprises:
directing the 3D scanning device to scan the surface of the reference object to produce the initial datum geometry reference scan prior to securing the ceramic or refractory mold or crucible in place on the support;
directing the 3D scanning device to scan the outer surface of the target region of the ceramic or refractory oxide mold or crucible to generate a corresponding 3D structure of the target region; or directing the 3D scanning device to scan the surface of the reference object to produce the initial datum geometry reference scan prior to secure the ceramic or refractory oxide mold or crucible in place on the support, and thereafter to scan the outer surface of the target region of the ceramic or refractory oxide mold or crucible to generate the corresponding 3D structure when the ceramic or refractory oxide mold or crucible is in place on the support.
39. The method according to claim 20, wherein operating the 3D
scanning device in conjunction with the computer component of the system in order to create the 3D structure difference map comprises:
using the 3D scanning device of the system or a different 3D scanning device to scan the surface of the reference object to generate the 3D
structure of the reference object;
using the 3D scanning device of the system to scan the outer surface of the target region of the ceramic or refractory oxide mold or crucible to generate the 3D
structure of said target region; and using the computer component to create the 3D structure difference map to determine whether the ceramic or refractory oxide mold or crucible fails within or outside of the desired structural integrity parameter range.
40. The method according to claim 39, wherein the reference object comprises either the mount portion of the fixture or a fugitive pattern of the ceramic or refractory oxide mold or crucible.
41. The method according to claim 20, wherein operating the 3D
scanning device in conjunction with the computer component of the system in order to create the 3D structure difference map comprises:
providing a computer aided design (CAD) model of the inner surface of a nominal model of the ceramic or refractory oxide mold or crucible;
using the 3D scanning device of the system to scan the outer surface of the target region of the ceramic or refractory oxide mold or crucible to generate the 3D
structure of said target region; and using the computer component to create the 3D structure difference map to determine whether the ceramic or refractory oxide mold or crucible fails within or outside of the desired structural integrity parameter range.
42. A method for non-destructive evaluation of a mold or crucible, said method comprising the steps of:
providing a system for non-destructive evaluation comprising:
a support comprising a fixture for securing a ceramic or refractory oxide mold or crucible in place for non-destructive evaluation, said fixture comprising a mount portion onto which the ceramic or refractory oxide mold or crucible is secured;
a three-dimensional (3D) scanning device for scanning an outer surface of a target region of the ceramic or refractory oxide mold or crucible in order to generate a 3D structure of the scanned outer surface of the target region;
and a computer component operably connected to the 3D scanning device and effective to create a difference map between the 3D structure of the scanned outer surface of the target region of the ceramic or refractory oxide mold or crucible and a 3D structure of a reference object corresponding to an inner surface of a nominal model of the same target region of the ceramic or refractory oxide mold or crucible, wherein said difference map indicates whether the ceramic or refractory oxide mold or crucible falls within or outside a desired structural integrity parameter range;
securing the mold or crucible to the support of the system; and operating the three-dimensional (3D) scanning device in conjunction with the computer component of the system in order to create a 3D structure difference map that indicates whether the mold or crucible falls within or outside a desired structural integrity parameter range, wherein the 3D structure difference map shows deviations between a 3D
structure generated by scanning an outer surface of a target region of the mold or crucible while secured on the support of the system and a 3D structure of a reference object corresponding to an inner surface of a nominal model of the same target region of the mold or crucible, wherein the method is performed on a plurality of different molds or crucibles using the same 3D structure of the reference object.
43. The method according to claim 20 further comprising:
using a robotic apparatus for placing the ceramic or refractory oxide mold or crucible on the support and for removing the ceramic or refractory oxide mold or crucible from the support.
CA2911765A 2013-05-10 2014-05-08 Systems and methods for non-destructive evaluation of molds and crucibles used in investment casting Expired - Fee Related CA2911765C (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/891,624 2013-05-10
US13/891,624 US9721044B2 (en) 2013-05-10 2013-05-10 Systems and methods for non-destructive evaluation of molds and crucibles used in investment casting
PCT/US2014/037276 WO2014182886A1 (en) 2013-05-10 2014-05-08 Systems and methods for nondestructive evaluation of molds and crucibles used in investment casting

Publications (2)

Publication Number Publication Date
CA2911765A1 CA2911765A1 (en) 2014-11-13
CA2911765C true CA2911765C (en) 2018-03-13

Family

ID=51022418

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2911765A Expired - Fee Related CA2911765C (en) 2013-05-10 2014-05-08 Systems and methods for non-destructive evaluation of molds and crucibles used in investment casting

Country Status (7)

Country Link
US (1) US9721044B2 (en)
EP (1) EP2994719B1 (en)
JP (1) JP6254260B2 (en)
CN (1) CN105393081B (en)
BR (1) BR112015028158A2 (en)
CA (1) CA2911765C (en)
WO (1) WO2014182886A1 (en)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8932518B2 (en) 2012-02-29 2015-01-13 General Electric Company Mold and facecoat compositions
DE102012215215A1 (en) * 2012-08-27 2014-05-28 Inb Vision Ag Method and device for detecting deviations of a surface of an object
US9900585B2 (en) * 2013-09-18 2018-02-20 Matter and Form Inc. Device, system and method for three-dimensional modeling
US9511417B2 (en) 2013-11-26 2016-12-06 General Electric Company Silicon carbide-containing mold and facecoat compositions and methods for casting titanium and titanium aluminide alloys
US9435889B2 (en) * 2013-12-14 2016-09-06 Process Metrix Caster mold measurements using a scanning range finder
US11023934B1 (en) * 2014-10-30 2021-06-01 Desprez, Llc Business variable optimization for manufacture or supply of designed products
US9984494B2 (en) * 2015-01-26 2018-05-29 Uber Technologies, Inc. Map-like summary visualization of street-level distance data and panorama data
CN105865368B (en) * 2016-05-06 2019-01-11 浙江大学 A kind of pressure vessel form variations detection method based on 3 D laser scanning
EP3252458A1 (en) * 2016-06-01 2017-12-06 Hijos de Jose Sivo, S.L. System and method for digitalizing tridimensional objects
US10166700B2 (en) * 2016-06-15 2019-01-01 Toyota Motor Engineering & Manufacturing North America, Inc. Methods for determining mold replacement timing in slush mold processing
WO2018211879A1 (en) * 2017-05-16 2018-11-22 新東工業株式会社 Surface treatment processing method and surface treatment processing device
EP3811288A4 (en) * 2018-06-22 2022-03-16 Raytheon Technologies Corporation Systems and methods for automated adaptive manufacturing of airfoil castings
US11408836B2 (en) * 2019-04-01 2022-08-09 General Electric Company Method for inspecting components using computed tomography
ES2903199T3 (en) * 2019-04-09 2022-03-31 Rosen Swiss Ag Method for determining the geometry of a defective point and for determining a load capacity limit
CN114008448B (en) 2019-04-28 2024-07-02 应达公司 Imaging and processing of refractory life cycle wear in an electric induction heating furnace
JP7338534B2 (en) 2020-03-30 2023-09-05 新東工業株式会社 Display controller and control program
JP7363638B2 (en) * 2020-03-30 2023-10-18 新東工業株式会社 Display control device and control program
US11893723B2 (en) 2020-03-30 2024-02-06 Sintokogio, Ltd. Inspection result display device and storage medium
DE102021107643A1 (en) 2020-03-30 2021-09-30 Sintokogio, Ltd. Display control device and storage medium
CN111735411B (en) * 2020-07-15 2023-01-06 动联(山东)电子科技有限公司 Volume scanner of quick installation
EP4330627A1 (en) * 2021-04-26 2024-03-06 2872475 Ontario Limited Vehicle damage detection system and method

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4352060A (en) * 1980-07-01 1982-09-28 Viak Ab Apparatus for measuring the interior dimensions of a cast iron mold
JP2859124B2 (en) 1994-03-30 1999-02-17 本田技研工業株式会社 Surface strain judgment method
JP3194518B2 (en) 1997-12-11 2001-07-30 富士通株式会社 Semiconductor device manufacturing equipment
JPH10185545A (en) 1996-12-27 1998-07-14 Shinetsu Eng Kk Shape measuring instrument for quartz crucible
US5848115A (en) * 1997-05-02 1998-12-08 General Electric Company Computed tomography metrology
JP3505114B2 (en) 1999-09-10 2004-03-08 松下電器産業株式会社 Single lens, mold, mold processing method, and optical pickup device using single lens
US6631752B2 (en) 2000-06-29 2003-10-14 Diecast Software Inc. Mathematically determined solidification for timing the injection of die castings
JP2003344026A (en) 2002-05-27 2003-12-03 Mitsubishi Heavy Ind Ltd Computer program and method for inspecting hollow vane
US20050159840A1 (en) * 2004-01-16 2005-07-21 Wen-Jong Lin System for surface finishing a workpiece
US20060176491A1 (en) 2004-12-22 2006-08-10 Hall William J Device and method for non-contact scanning of contact lens mold geometry
US7573974B2 (en) * 2006-02-22 2009-08-11 Novartis Ag Device and method for non-contact scanning of contact lens and contact lens mold geometry
JP2007307580A (en) * 2006-05-18 2007-11-29 Sintokogio Ltd Measuring method of mold cavity surface, and storage medium therefor
US8578581B2 (en) * 2007-04-16 2013-11-12 Pratt & Whitney Canada Corp. Method of making a part and related system
US8048365B2 (en) * 2007-04-30 2011-11-01 General Electric Company Crucibles for melting titanium alloys
US7824730B2 (en) 2007-08-31 2010-11-02 United Technologies Corporation Method and apparatus for measuring coating thickness with a laser
JP2009166136A (en) 2008-01-10 2009-07-30 Nano-Optonics Research Institute Grinding device to manufacture optical element, manufacturing method of optical element and precision measuring device for precisely measuring shape/dimension of metallic mold to manufacture optical element or optical element
EP2312267A1 (en) 2009-10-19 2011-04-20 Siemens Aktiengesellschaft Device and method for measuring thickness of coating with laser triangulation

Also Published As

Publication number Publication date
JP6254260B2 (en) 2017-12-27
US9721044B2 (en) 2017-08-01
CN105393081A (en) 2016-03-09
EP2994719B1 (en) 2019-09-04
BR112015028158A2 (en) 2017-07-25
EP2994719A1 (en) 2016-03-16
US20140336806A1 (en) 2014-11-13
CN105393081B (en) 2019-01-25
JP2016519312A (en) 2016-06-30
WO2014182886A1 (en) 2014-11-13
CA2911765A1 (en) 2014-11-13

Similar Documents

Publication Publication Date Title
CA2911765C (en) Systems and methods for non-destructive evaluation of molds and crucibles used in investment casting
EP1739409A1 (en) Thermal imaging and laser scanning systems and methods for determining the location and angular orientation of a hole with an obstructed opening residing on a surface of an article
US7333218B2 (en) Systems and methods for determining the location and angular orientation of a hole with an obstructed opening residing on a surface of an article
JP5078296B2 (en) Photogrammetry apparatus and photogrammetry system
CN109115128B (en) A kind of welding bead three-dimensional appearance testing method based on area-structure light
US9404843B2 (en) System and method for determining wear of a worn surface
US11410298B2 (en) System and method for determining part damage
Burghardt et al. Robot-operated inspection of aircraft engine turbine rotor guide vane segment geometry
CN115578429B (en) Mold online precision detection method based on point cloud data
CN108765565A (en) A kind of tri-dimensional entity modelling method of FOD damages
CN108593710B (en) Thermal imaging detection system and method for surface defects of high-reflectivity material
Blug et al. Application of high‐performance DIC for a comprehensive evaluation of biaxial fatigue crack growth experiments
CN117092142A (en) Hollow turbine blade detection method, system and equipment
CN108050935B (en) Method for rapidly detecting error modulus of precision front axle forging piece on line
Bračun et al. A method for surface quality assessment of die-castings based on laser triangulation
Middendorf et al. In situ wear measurement of hot forging dies using robot aided endoscopic fringe projection
Keller et al. Parameters influencing the precision of SLM production
EP3626388B1 (en) Method of forming cooling holes
Weckenmann et al. Testing formed sheet metal parts using fringe projection and evaluation by virtual distortion compensation
Petrov et al. Applying 3D-scan systems rangevision for precision preparing of polygonal 3D-models
Karczewski et al. Application of reverse engineering for identification of damage and support the reparation of the vehicles
Kanun Using photogrammetric modeling in reverse engineering applications: Damaged turbocharger example
Żaba et al. Application of non-destructive methods to quality assessment of pattern assembly and ceramic mould in the investment casting elements of aircraft engines
Ferreira Automatic volume inspection for glass blow moulds
Nowacki et al. The use of 3D scanning technology in measurements of welding distortions

Legal Events

Date Code Title Description
EEER Examination request

Effective date: 20151105

MKLA Lapsed

Effective date: 20210510